View from above orbital plane
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View from above satellite
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Ground track
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The orbit data is extracted from the following two-line orbital elements,
1 24278U 96046B 14204.08201360 -.00000015 00000-0 21237-4 0 4260
2 24278 098.5122 212.9895 0350271 204.3401 191.3205 13.53026419885523
| Epoch (UTC): | 23 July 2014 01:58:05 |
| Eccentricity: | 0.0350271 |
| inclination: | 98.5122° |
| perigee height: | 800 km |
| apogee height: | 1322 km |
| right ascension of ascending node: | 212.9895° |
| argument of perigee: | 204.3401° |
| revolutions per day: | 13.53026419 |
| mean anomaly at epoch: | 191.3205° |
| orbit number at epoch: | 88552 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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